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Title: In space startup method for nuclear fusion rocket engines

Abstract

The invention is for a startup system for nuclear fusion engines in space. The combustion of hydrogen and oxygen produces heat that is used by a heat engine to produce electricity. This can be supplemented by electricity from other operating engines. The exhaust from the combustion is condensed and electrolyzed to produce hydrogen and oxygen once the engine is in operation. This provides a constant source of energy for future startups. The engine is started up at partial power in electricity generation mode and this power replaces the power from the combustion as it grows. The combustor uses the same heat engine as the nuclear engine uses for power generation.

Inventors:
; ; ;
Issue Date:
Research Org.:
Princeton Plasma Physics Laboratory (PPPL), Princeton, NJ (United States)
Sponsoring Org.:
USDOE
OSTI Identifier:
1525050
Patent Number(s):
10229756
Application Number:
14/466,425
Assignee:
Princeton Satellite Systems, Inc. (Plainsboro, NJ); The Trustees of Princeton University (Princeton, NJ)
Patent Classifications (CPCs):
B - PERFORMING OPERATIONS B64 - AIRCRAFT B64G - COSMONAUTICS
F - MECHANICAL ENGINEERING F02 - COMBUSTION ENGINES F02B - INTERNAL-COMBUSTION PISTON ENGINES
DOE Contract Number:  
AC02-09CH11466
Resource Type:
Patent
Resource Relation:
Patent File Date: 2014-08-22
Country of Publication:
United States
Language:
English
Subject:
46 INSTRUMENTATION RELATED TO NUCLEAR SCIENCE AND TECHNOLOGY; 08 HYDROGEN; 30 DIRECT ENERGY CONVERSION

Citation Formats

Paluszek, Michael A., Ham, Eric M., Razin, Yosef, and Cohen, Samuel A. In space startup method for nuclear fusion rocket engines. United States: N. p., 2019. Web.
Paluszek, Michael A., Ham, Eric M., Razin, Yosef, & Cohen, Samuel A. In space startup method for nuclear fusion rocket engines. United States.
Paluszek, Michael A., Ham, Eric M., Razin, Yosef, and Cohen, Samuel A. Tue . "In space startup method for nuclear fusion rocket engines". United States. https://www.osti.gov/servlets/purl/1525050.
@article{osti_1525050,
title = {In space startup method for nuclear fusion rocket engines},
author = {Paluszek, Michael A. and Ham, Eric M. and Razin, Yosef and Cohen, Samuel A.},
abstractNote = {The invention is for a startup system for nuclear fusion engines in space. The combustion of hydrogen and oxygen produces heat that is used by a heat engine to produce electricity. This can be supplemented by electricity from other operating engines. The exhaust from the combustion is condensed and electrolyzed to produce hydrogen and oxygen once the engine is in operation. This provides a constant source of energy for future startups. The engine is started up at partial power in electricity generation mode and this power replaces the power from the combustion as it grows. The combustor uses the same heat engine as the nuclear engine uses for power generation.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2019},
month = {3}
}

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